Open AccessOptimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system
Author(s) -
Ю. М. Заболотнов,
А. А. Лобанков
Publication year - 2016
Publication title -
vestnik samarskogo universiteta. aèrokosmičeskaâ tehnika, tehnologii i mašinostroenie
Language(s) - English
Resource type - Journals
eISSN - 2541-7533
pISSN - 2542-0453
DOI - 10.18287/2412-7329-2016-15-1-46-54
Subject(s) - nutation , spacecraft , physics , optimal control , precession , control theory (sociology) , orbital motion , orbit (dynamics) , center of mass (relativistic) , angular velocity , classical mechanics , computer science , angular momentum , aerospace engineering , mathematics , control (management) , engineering , mathematical optimization , astronomy , artificial intelligence , energy–momentum relation